TM 55-1560-307-13&P
Table 2-1. ERFS Components (Cont)
NOMENCLATURE
PART NUMBER
NSN
QTY
Hose Assy
AE706285-6
4720-01-214-1001
1
Hose Assy
MS28741-24D-0160
. . .
1
Hose Assy
390A-16D-0720
. . .
4
Identical Tee
180-950248-16D-0360
Hose Assy
. . .
1
Panel Assy (FMCP)
85SDSCC-D-0007-100
. . .
1
Plywood Deck
85SDSCC-D-0007-187
. . .
8
Shoring
Pump Assy
85SDSCC-D-0007-101
. . .
4
Quick Disconnect
114PS491-2
4730-01-140-6760
2
Reducer, Tube
MS24399D28
4730-01-262-8293
1
Strap, Webbing
SP4212-1
1670-00-725-1437
38
Strap, Webbing
B-D-10000 R/0-234-HH-24
5340-01-233-3063
8
Wrench
1232
5120-00-203-4812
1
Wrench
1248
5120-00-203-4804
1
Wrench
1244
5120-00-203-4806
1
Wrench
1240
5120-00-203-4808
1
Wrench
1252
5120-00-203-4802
1
Section II. INSPECTING THE EQUIPMENT
2-4. INSPECTION. Inspect the ERFS components as
follows:
CAUTION
A daily visual inspection shall be
made of the subject installation to
ensure that no progressive structural
deterioration is occurring, that there
is no loss of security, and that no
damage to the host helicopter, tank
fittings, tiedown straps, etc., exist.
Any occurrence of the preceding
shall be corrected prior to further
flight operations.
a. Initial Installation. The ERFS will be inspected
after initial installation in the aircraft.
b. When system components have been out of
service for a period of 7 days or more.
c. When maintenance has been preformed on any
part or component of the system to correct a
malfunction.
d. When the ERFS tank system has been purged
in accordance with instructions provided in Chapter 3,
Section V, para 3-25 of this manual.
e. Before each flight, check system in accordance
with the PMCS, Table 2-6.
f. Immediately after fueling system, inspect for
leaks.
2-2
